Deep Space Transport


The Deep Space Transport, also called Mars Transit Vehicle, is a crewed interplanetary spacecraft concept by NASA to support science exploration missions to Mars of up to 1,000 days. It would be composed of two elements: an Orion capsule and a propelled habitation module. As of late 2019, the DST is still a concept to be studied, and NASA has not officially proposed the project in an annual U.S. federal government budget cycle.
The DST vehicle would depart and return from the Lunar Gateway to be serviced and reused for a new Mars mission.

Architecture overview

Both the Gateway and the DST would be fitted with the International Docking System Standard. The DST spacecraft would comprise two elements: an Orion capsule and a habitation module that would be propelled by both electric propulsion and chemical propulsion, and carry a crew of four in a medium-sized habitat. The fully assembled spacecraft with the Orion capsule mated, would have a mass of about 100 metric tons. The spacecraft's habitat portion will likely be fabricated using tooling and structures developed for the SLS propellant tank; it would be in diameter and in length.
The habitat portion of the DST spacecraft may also be equipped with a laboratory with research instrumentation for physical sciences, electron microscopy, chemical analyses, freezers, medical research, small live animal quarters, plant growth chambers, and 3D printing. External payloads might include cameras, telescopes, detectors, and a robotic arm.
Its initial target for exploration is Mars, and other suggested destinations are Venus, and a sample return from a large asteroid. If the DST spacecraft were to orbit Mars, it would enable opportunities for real-time remote operation of equipment on the Martian surface, such as a human-assisted Mars sample return.
It would use a lunar flyby to build up speed and then using solar electric propulsion it would accelerate into a heliocentric orbit. There it would complete its transit to Mars or other possible destinations. It would use chemical propulsion to enter Mars orbit. Crews could perform remote observations or depart for the surface during a 438-day window. The vehicle would depart Mars orbit via a chemical burn. It would use a mix of SEP and lunar gravity assists to recapture into Earth's sphere of influence.
Fully assembled DSTEstimated mass
Orion capsule
10.3
Habitat21.9
Cargo26.5
Solar electric propulsion system
including xenon propellant		24
Chemical propellant16
Estimated total98.7

Suggested timeline

If funded, the DST would be launched toward the Lunar Gateway in one SLS cargo flight, probably in 2027. The spacecraft would be expected to undergo 100–300 days of DST Habitat crewed operation before it starts a one-year long flight test in cislunar space in 2029 at the earliest. It would be designed to transport a crew to orbit Mars, but not land, in the 2030s. Its first mission would likely involve a Venus flyby and a short stay around Mars. Additional developments and vehicles would be required for a Mars human surface mission.
In August 2019, the Science and Technology Policy Institute delivered a report commissioned by NASA in 2017 specifically for a technical and financial assessment of "a Mars human space flight mission to be launched in 2033" using the DST. The report concluded that "even without budget constraints, a Mars 2033 orbital mission cannot be realistically scheduled under NASA's current and notional plans," and that "the analysis suggests that a Mars orbital mission could be carried out no earlier than the 2037 orbital window without accepting large technology development, schedule delay, cost overrun, and budget shortfall risks." A mission to Mars launching in 2033, the report concluded, would need to have life support systems and propulsion tested by 2022, which is unlikely. The report estimated that the total cost of the elements needed for the Mars mission, including SLS, Orion, Gateway, DST and other logistics, at $120.6 billion through fiscal year 2037.